Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag14-il-50000 Airfoil,ag14-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,34.8193 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-ag14-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.750,-0.5471,0.10787,0.10137,0.0153,1.0000,0.1712 -7.500,-0.5334,0.10277,0.09629,0.0164,1.0000,0.1777 -7.250,-0.5383,0.10140,0.09503,0.0107,1.0000,0.1854 -7.000,-0.5228,0.09617,0.08981,0.0138,1.0000,0.1947 -6.500,-0.5081,0.08910,0.08287,0.0099,1.0000,0.2170 -6.250,-0.4982,0.08552,0.07934,0.0091,1.0000,0.2321 -6.000,-0.4882,0.08212,0.07592,0.0079,1.0000,0.2501 -5.750,-0.4791,0.07885,0.07271,0.0040,1.0000,0.2694 -5.500,-0.4661,0.07495,0.06886,0.0065,1.0000,0.2880 -5.250,-0.4549,0.07159,0.06553,0.0047,1.0000,0.3118 -5.000,-0.4427,0.06824,0.06223,0.0045,1.0000,0.3387 -4.750,-0.4304,0.06478,0.05883,0.0064,1.0000,0.3672 -4.500,-0.4182,0.06145,0.05556,0.0091,1.0000,0.3990 -4.000,-0.2706,0.03995,0.03206,-0.0437,1.0000,0.1347 -3.750,-0.2321,0.03477,0.02597,-0.0470,1.0000,0.1159 -3.500,-0.2003,0.03135,0.02190,-0.0482,1.0000,0.1168 -3.250,-0.1719,0.02836,0.01866,-0.0484,1.0000,0.1217 -3.000,-0.1410,0.02561,0.01542,-0.0484,1.0000,0.1243 -2.750,-0.1116,0.02338,0.01278,-0.0481,1.0000,0.1365 -2.500,-0.0832,0.02148,0.01067,-0.0475,1.0000,0.1607 -2.250,-0.0561,0.01968,0.00899,-0.0466,1.0000,0.2086 -2.000,-0.0278,0.01735,0.00733,-0.0459,1.0000,0.3467 -1.750,-0.0101,0.01371,0.00587,-0.0411,1.0000,1.0000 -1.500,0.0182,0.01370,0.00516,-0.0410,1.0000,1.0000 -1.250,0.0450,0.01370,0.00467,-0.0408,1.0000,1.0000 -1.000,0.0712,0.01373,0.00434,-0.0405,1.0000,1.0000 -0.750,0.0971,0.01377,0.00411,-0.0402,1.0000,1.0000 -0.500,0.1227,0.01383,0.00395,-0.0399,1.0000,1.0000 -0.250,0.1481,0.01391,0.00386,-0.0396,1.0000,1.0000 0.000,0.1733,0.01401,0.00380,-0.0393,1.0000,1.0000 0.250,0.1983,0.01414,0.00383,-0.0390,1.0000,1.0000 0.500,0.2230,0.01430,0.00393,-0.0388,1.0000,1.0000 0.750,0.2474,0.01450,0.00410,-0.0387,1.0000,1.0000 1.000,0.2715,0.01474,0.00434,-0.0386,1.0000,1.0000 1.250,0.2952,0.01505,0.00467,-0.0386,1.0000,1.0000 1.500,0.3185,0.01545,0.00511,-0.0388,1.0000,1.0000 1.750,0.3409,0.01598,0.00569,-0.0393,1.0000,1.0000 2.000,0.3620,0.01668,0.00648,-0.0401,1.0000,1.0000 2.250,0.3814,0.01766,0.00756,-0.0415,1.0000,1.0000 2.500,0.4836,0.01826,0.00857,-0.0566,0.9439,1.0000 2.750,0.5603,0.01809,0.00874,-0.0639,0.8852,1.0000 3.000,0.5990,0.01804,0.00889,-0.0631,0.8253,1.0000 3.250,0.6235,0.01821,0.00902,-0.0596,0.7678,1.0000 3.500,0.6442,0.01858,0.00927,-0.0557,0.7112,1.0000 3.750,0.6647,0.01909,0.00962,-0.0523,0.6551,1.0000 4.000,0.6858,0.01973,0.01008,-0.0493,0.5996,1.0000 4.250,0.7077,0.02050,0.01075,-0.0469,0.5447,1.0000 4.500,0.7301,0.02139,0.01146,-0.0448,0.4907,1.0000 4.750,0.7528,0.02241,0.01234,-0.0430,0.4384,1.0000 5.000,0.7758,0.02354,0.01332,-0.0413,0.3898,1.0000 5.250,0.7990,0.02481,0.01451,-0.0399,0.3443,1.0000 5.500,0.8224,0.02620,0.01582,-0.0387,0.3031,1.0000 5.750,0.8460,0.02780,0.01744,-0.0375,0.2676,1.0000 6.000,0.8698,0.02966,0.01942,-0.0365,0.2361,1.0000 6.250,0.8929,0.03154,0.02138,-0.0354,0.2072,1.0000 6.500,0.9161,0.03411,0.02418,-0.0345,0.1850,1.0000 6.750,0.9385,0.03632,0.02632,-0.0335,0.1623,1.0000 7.000,0.9591,0.03981,0.03039,-0.0325,0.1467,1.0000 7.250,0.9783,0.04357,0.03455,-0.0316,0.1339,1.0000 7.500,0.9948,0.04716,0.03852,-0.0308,0.1207,1.0000 7.750,1.0041,0.05329,0.04553,-0.0306,0.1179,1.0000 8.000,1.0083,0.05996,0.05292,-0.0312,0.1175,1.0000 8.250,1.0072,0.06690,0.06032,-0.0325,0.1181,1.0000 8.500,1.0025,0.07387,0.06759,-0.0345,0.1193,1.0000 8.750,0.9966,0.08065,0.07445,-0.0368,0.1206,1.0000 9.000,0.9912,0.08723,0.08112,-0.0390,0.1216,1.0000 9.250,0.9879,0.09366,0.08772,-0.0409,0.1225,1.0000 9.500,0.8843,0.12445,0.11801,-0.0853,0.3004,1.0000